Methods and devices for supporting of variety of different pre-cured composite stringers

ABSTRACT

Provided are methods and devices for supporting of variety of different pre-cured composite stringers after forming and prior to curing. A post-forming processing device comprises a base with a channel for receiving hat portions of different stringers. The device also comprises a support structure, at least partially extending within the channel. The support structure is configured to conform to different hat portions and to retain the shape of these hat portions. For example, the support structure is made from a flexible material, which conforms to any shape variations. In some examples, the support structure is made from a jamming material that is reshaped together with each of the pre-cured composite stringers. A post-forming processing device is used for supporting different pre-cured composite stringers while various operations are performed on these stringers, such as stringer trimming, inspection, installation of bladders and noodles, and the like.

CROSS-REFERENCE TO RELATED APPLICATIONS

This application is a divisional of U.S. patent application Ser. No.16/802,321, entitled: “METHODS AND DEVICES FOR SUPPORTING OF VARIETY OFDIFFERENT PRE-CURED COMPOSITE STRINGERS”, filed on Feb. 26, 2020, whichis incorporated herein by reference in its entirety for all purposes.

BACKGROUND

Aircraft utilize various components, such as stringers, to resistbending, torsional, shear, and direct loads. Stringers are typicallyformed from a lightweight composite using, e.g., a tape or fabric withfibers embedded in a resin matrix. For example, a composite layup isprocessed in a forming tool to define the shape. The shaped component isthen transferred to a curing device for curing. Up until the curing iscompleted, the stringer requires sufficient support to retain its shape.This shape is often defined by in-plane and/or out-of-plane bends inaddition to cross-sectional profiles that vary from one stringer toanother. Furthermore, the shaped stringer may subjected to variousoperations, prior to the curing, such as trimming, inspection,installation of additional components, and the like. This support to theuncured stringer is typically provided by either the forming tool or thecuring tool, which limits the throughput by either one of these toolsand slows down the overall processing speed.

What is needed are new methods and devices for supporting of variety ofdifferent pre-cured composite stringers after forming and prior tocuring.

SUMMARY

Provided are methods and devices for supporting of variety of differentpre-cured composite stringers after forming and prior to curing. Apost-forming processing device comprises a base with a channel forreceiving hat portions of different stringers. The device also comprisesa support structure, at least partially extending within the channel.The support structure is configured to conform to different hat portionsand to retain the shape of these hat portions. For example, the supportstructure is made from a flexible material, which conforms to any shapevariations. In some examples, the support structure is made from ajamming material that is reshaped together with each of the pre-curedcomposite stringers. A post-forming processing device is used forsupporting different pre-cured composite stringers while variousoperations are performed on these stringers, such as stringer trimming,inspection, installation of bladders and noodles, and the like.

In some examples, a post-forming processing device for supportingpre-cured composite stringers is provided. The composite stringerscomprise hat portions, having cross-sections, different among thepre-cured composite stringers. The post-forming processing devicecomprises a base, a support structure, and a cover. The base comprises achannel, having a channel width and a channel height. The channel widthis larger than the width of the hat portions of the pre-cured compositestringers. The channel height is larger than the heights of the hatportions of the pre-cured composite stringers. The support structure atleast partially extends within the channel and along a length of thechannel. The support structure is configured to conform to each of thehat portions and to retain a cross-sectional shape of each of the hatportions when a corresponding one of the pre-cured composite stringersis supported by the post-forming processing device. The cover isconfigured to attach to the base, such that the corresponding one of thepre-cured composite stringers is positioned between the cover and thebase while supported by the post-forming processing device.

Also provided is a method of fabricating a composite stringer. Themethod comprises forming a pre-cured composite stringer on a formingdevice, the pre-cured composite stringer comprising a hat portion andtransferring the pre-cured composite stringer from the forming device toa post-forming processing device. The post-forming processing devicecomprises a base, comprising a channel, and a support structure, atleast partially extending within the channel and along a length of thechannel and conforming to the hat portion and retaining across-sectional shape of the hat portion. The method further comprisesinstalling a bladder on the pre-cured composite stringer, while thepre-cured composite stringer is positioned on the post-formingprocessing device. The method comprises installing a noodle at aninterface between the bladder and the pre-cured composite stringer andwithin a plane of the support surface of the base, while the pre-curedcomposite stringer is positioned on the post-forming processing device.The method further comprises transferring the pre-cured compositestringer together with the bladder and the noodle from the post-formingprocessing device to a curing device and curing the pre-cured compositestringer on the curing device, thereby forming the composite stringer.

In some examples, a method comprises transferring a pre-cured compositestringer, comprising a hat portion, to a post-forming processing device.The post-forming processing device comprises a base, comprising achannel, and a support structure, at least partially extending withinthe channel and along a length of the channel and conforming to the hatportion of the pre-cured composite stringer and retaining across-sectional shape of the hat portion of the pre-cured compositestringer. The method proceeds with removing the pre-cured compositestringer from the post-forming processing device and transferring anadditional pre-cured composite stringer, comprising an additional hatportion, to the post-forming processing device. The support structure ofthe post-forming processing device conforms to the additional hatportion of the additional pre-cured composite stringer and retains across-sectional shape of the additional hat portion of the additionalpre-cured composite stringer, different from the cross-sectional shapeof the hat portion of the pre-cured composite stringer.

BRIEF DESCRIPTION OF THE DRAWINGS

FIG. 1A a process flowchart of fabricating a composite stringer.

FIG. 1B is a process flowchart of fabricating a composite stringer, inaccordance with other examples of the present disclosure.

FIGS. 1C, 1D, and 1E are different examples of composite stringers.

FIG. 2A is a schematic cross-sectional view of a post-forming processingdevice, comprising a flexible support structure, in accordance with someexamples of the present disclosure.

FIG. 2B is a schematic cross-sectional view of the post-formingprocessing device in FIG. 2A, showing the flexible support structureconforming to the hat portion of a pre-cured composite stringer, inaccordance with some examples of the present disclosure.

FIG. 2C is a schematic cross-sectional view of the post-formingprocessing device in FIGS. 2A and 2B, showing the cover sealed againstthe base and enclosing the pre-cured composite stringer, in accordancewith some examples of the present disclosure.

FIG. 2D is a schematic cross-sectional view of a post-forming processingdevice, comprising a flexible support structure and a flexible insert,both positioned in a channel, in accordance with some examples of thepresent disclosure.

FIG. 2E is a schematic cross-sectional view of a post-forming processingdevice, illustrating a tapered channel, in accordance with some examplesof the present disclosure.

FIG. 2F is schematic top view of a post-forming processing device,illustrating bladder seals, in accordance with some examples of thepresent disclosure.

FIG. 3A is a schematic cross-sectional view of a post-forming processingdevice, comprising a pre-formed support structure made from a jammingmaterial, in accordance with some examples of the present disclosure.

FIG. 3B is a schematic cross-sectional view of the post-formingprocessing device in FIG. 3A, showing the flexible support structureengaging a pre-cured composite stringer, in accordance with someexamples of the present disclosure.

FIG. 3C is a schematic cross-sectional view of the post-formingprocessing device in FIGS. 3A and 3B, showing the cover sealed againstthe base and enclosing the pre-cured composite stringer, in accordancewith some examples of the present disclosure.

FIG. 4 is a process flowchart corresponding to a method of fabricating acomposite stringer, in accordance with some examples of the presentdisclosure.

FIG. 5A is a schematic illustration of a laminated layup, disposed on aprocessing surface of a forming base and extending over a cavity, inaccordance with some examples of the present disclosure.

FIG. 5B is a schematic illustration of the laminated layup, shaped intoa pre-cured composite stringer, by the forming device, in accordancewith some examples of the present disclosure.

FIG. 5C is a schematic illustration of the pre-cured composite stringer,supported by a post-forming processing device, in accordance with someexamples of the present disclosure.

FIG. 5D is a schematic illustration of a bladder, installed into thepre-cured composite stringer, while the pre-cured composite stringer issupported by the post-forming processing device, in accordance with someexamples of the present disclosure.

FIG. 5E is a schematic illustration of a noodle installed, at aninterface between the bladder and the pre-cured composite stringer,while the pre-cured composite stringer is supported by the post-formingprocessing device, in accordance with some examples of the presentdisclosure.

FIG. 5F is a schematic illustration of a cover sealed against the baseof the post-forming processing device, in accordance with some examplesof the present disclosure.

FIG. 5H is a schematic illustration of the pre-cured composite stringertransferred together with the bladder and the noodle to a curing device,in accordance with some examples of the present disclosure.

FIG. 5I is a schematic illustration of a composite stringer beingremoved from the curing device, in accordance with some examples of thepresent disclosure.

FIG. 5J is a schematic illustration of an additional pre-cured compositestringer, supported by a post-forming processing device, in accordancewith some examples of the present disclosure.

FIGS. 6A and 6B are top schematic views of a post-forming processingdevice, showing in-plane bending, in accordance with some examples ofthe present disclosure.

FIG. 7 is a process flowchart corresponding to a method of supporting apre-cured composite stringer in a post-forming processing device, inaccordance with some examples of the present disclosure.

FIG. 8 is a process flowchart corresponding to a method formanufacturing and service the aircraft.

FIG. 9 illustrates a block diagram of an example of an aircraft, inaccordance with some examples of the present disclosure.

DETAILED DESCRIPTION

In the following description, numerous specific details are set forth inorder to provide a thorough understanding of the presented concepts. Insome examples, the presented concepts are practiced without some or allof these specific details. In other instances, well known processoperations have not been described in detail so as to not unnecessarilyobscure the described concepts. While some concepts will be described inconjunction with the specific examples, it will be understood that theseexamples are not intended to be limiting.

Introduction

Composite stringers and other shaped composite structures are used formany applications, such as aircraft, land vehicles, and the like.Fabrication of these composite structures involves various handling andprocessing of pre-cured shaped components, such as trimming, inspection,bladder installations, and such. Prior to curing, these shapedcomponents require sufficient support to retain the shape, which can bechallenging due to differences in shapes and sizes of these pre-curedcomponents. For example, a modern aircraft uses hundreds of differentcomposite stringers, which have different sizes, cross-sectional shapes,in-plane bends, and/or out-of-plane bends. Providing a dedicated supportfor each type of these composite stringers is challenging and expensive,adding to an already large number of specialized tools used infabrication of composite stringers.

FIGS. 1A and 1B illustrate two process flowcharts representing differentexamples of fabrication a composite stringer and corresponding toolsused for various operations. FIGS. 1A and 1B are presented to providesome context and general overview of key components, tools, and steps.In both examples, the process starts with forming device 510 shapingcomposite layup 502, thereby forming pre-cured composite stringer 190.Curing device 540 then cures pre-cured composite stringer 190, therebyforming composite stringer 198. Pre-cured composite stringer 190 andcomposite stringer 198 have the generally same shape, but differentmaterial and mechanical properties. For example, the resin of pre-curedcomposite stringer 190 is not fully crosslinked or not as cross-inked asthe resin of composite stringer 198. As such, pre-cured compositestringer 190 is still able to change the shape and requires supportbefore curing.

Both forming device 510 and curing device 540 are specifically shaped toaccommodate a particular design of composite stringer 198. Therefore,either one or both of forming device 510 and curing device 540 can beused for supporting pre-cured composite stringer 190 after completingthe forming operation and before initiating the curing operation, whichcorresponds to the example shown in FIG. 1A. However, this approachoccupies one or both forming device 510 and curing device 540 foroperations that are not core functions of these devices. Furthermore,many of these operations and even storage of pre-cured compositestringer 190 may take significant periods of time. As a result, thethroughput of one or both forming device 510 and curing device 540 canbe limited by these intermediate operations and storage associated withpre-cured composite stringer 190.

Referring to FIG. 1B, post-forming processing device 100 is used toreceive pre-cured composite stringer 190 after pre-cured compositestringer 190 is formed/shaped. Post-forming processing device 100 isalso used to support pre-cured composite stringer 190 up until thecuring operation. Post-forming processing device 100 effectivelyrelieves forming device 510 and curing device 540, increasing theirprocessing throughputs. Post-forming processing device 100 is used forvarious operations, performed on pre-cured composite stringer 190, and,in some examples, for storing pre-cured composite stringer 190.

However, if a post-forming processing device is specifically andpermanently shaped for accommodating the shape of each specificcomposite stringer, then the numbers of such post-forming processingdevices would be the same as the number of different stringers. Thisapproach is not desirable from a space and cost savings perspective andcan complicate the overall process by requiring a large number ofadditional tools. Furthermore, post-forming processing devices, whichare specifically and permanently shaped, may not be always stackable dueto the design variations, which complicates their storage. It shouldalso be noted that the supply base is limited based on complexity of thepost-forming processing device. Also, 3-D geometry increases complexityfor shuttling the stringers around. Finally, 3-D geometry likelyincreases weight which will inhibit manual handling for a variety ofreasons including maintenance.

Design variations of composite stringers or, more specifically,different examples of pre-cured composite stringer 190 are shown inFIGS. 1C, 1D, and 1E. In each example, pre-cured composite stringer 190comprises flange portions 196, which define contact surface 197. Contactsurface 197 is used for connecting the composite stringer, formed frompre-cured composite stringer 190, to other components, e.g., a compositeskin of an aircraft. These other components define the shape of contactsurface 197. In some examples, contact surface 197 is planar.Alternatively, contact surface 197 and, more generally, the entirestringer has an out-of-plane bend.

Each of pre-cured composite stringers 190 also comprises hat portion191, which interconnects and is positioned between flange portions 196.Hat portion 191 extends away from contact surface 197, defining stringercavity 192. Hat portion 191 is defined by the height (H) of hat portion191, which is defined as a maximum deviation from contact surface 197.Hat portion 191 is also defined by the width (W) of hat portion 191,which is defined as the gap between flange portions 196.

Referring to FIG. 1C, in some examples, hat portion 191 is formed bystraight walls. Alternatively, in some examples, hat portion 191 isformed by a continuous curved wall, e.g., as shown in FIG. 1E. FIG. 1Dillustrates an example where hat portion 191 is formed by a combinationof straight and curved walls. FIGS. 1C, 1D, and 1E illustrate thatpre-cured composite stringers 190, shown in these figures, requiredifferent types of support from post-forming processing device 100.Furthermore, FIGS. 1C, 1D, and 1E illustrate that pre-cured compositestringers 190 are not stackable. Therefore, if permanently-rigidsupports are used for these pre-cured composite stringers, thesesupports will not be stackable either. For purposes of differentiatingpre-cured composite stringers, an example shown in FIG. 1E may bereferred to as additional pre-cured composite stringers 199. Processingdifferent types of pre-cured composite stringers using the samepost-forming processing device 100 is described below with reference toFIG. 4 .

Described methods and devices are used for supporting of variety ofdifferent pre-cured composite stringers, such as ones shown in FIGS.1A-1C. More specifically, the same post-forming processing device isconfigured to support pre-cured composite stringers with differentcross-sectional profiles of their hat portions. Specifically, apost-forming processing device comprises a channel and a supportstructure, at least partially extending within the channel. The supportstructure is configured to conform to each of differently shaped hatportions the pre-cured composite stringers and to retain the shape ofthese hat portions while providing the support. In some example, thesupport structure is made from a flexible material that conforms to anyshape of the hat portions. Alternatively, the support structure is madefrom a jamming material and is reshaped together with each of thepre-cured composite stringers.

Within examples of the present disclosure, the disclosed post-formingprocessing device is used for supporting different pre-cured compositestringers while various operations are performed on these stringers,such as stringer trimming, inspection, installation of bladders andnoodles, and the like. Furthermore, in some examples, the disclosedpost-forming processing device is used for storing pre-cured compositestringers. Overall, adding the disclosed post-forming processing deviceinto the overall process flow allows increasing processing throughputsof other devices, such as forming devices and curing devices. Overall,the disclosed post-forming processing devices provide high rateautomation of stringer installation by merging the gap between formingand curing devices with these post-forming processing devices.

The described methods also incorporate alignment fittings to ensure theproper alignment between the stringer and the bladder for dead endfittings. Offset of the bladder helps to provide proper support andfunctionality during cure. For example, in some instances, a bladder isterminated inside of the edge of the part. Specific examples includedoor structures, window structures, and convergence structures (e.g.,aircraft structures with pointy ends).

It should be noted that the cavity is tools used for forming stringer,accommodate both a stringer and a bladder. If the bladder does notextend past the stringer, the bladder will either interfere or leave anunacceptably large gap inside the tool. Since the bladder is aligned andlocked to the stringer at the kitting stage, it is beneficial for thatthe bladder be indexed in the correct position to avoid rework at laterstages.

Additionally, some bladders receive one or more layers of materialwrapped around these bladders prior to insertion to correspondingstringers. In some examples, this assembly includes a glass ply, alignedto the end of the stringers to add the corrosion protection inside thestringer. In other examples, this assembly includes a carbon wrap, whichadds strength to the stringer. In these later examples, the bladder wrapis aligned with the stringer.

Examples of Post-Forming Processing Device

FIG. 2A is a schematic cross-sectional view of post-forming processingdevice 100 for supporting pre-cured composite stringers 190, inaccordance with some examples. Post-forming processing device 100comprises base 110, support structure 120, and, optionally, cover 130.In some examples, post-forming processing device 100 does not have or,at least, is used in some operations without cover 130.

Base 110 is formed from a rigid material, such as carbon fiber,aluminum, a pultruded polyester/glass solution, and the like. Base 110comprises support surface 114, which faces cover 130, when cover 130 ispresent. Support surface 114 is configured to seal against cover 130and, in some examples, comprises one or more sealing features. Duringthe operation of post-forming processing device 100, support surface 114is used to support flange portions 196 of stringer 190, e.g., bycompressing flange portions 196 between support surface 114 and cover.In some examples, support surface 114 is planar. In general, supportsurface 114 conforms to the shape of flange portions 196 of stringer190.

Base 110 also comprises channel 112, partially extending through base110 and having opening 113. Opening 113 separates two portions ofsupport surface 114. As shown in FIG. 2A, channel 112 has a channelwidth (CW) and a channel height (CH). The channel width (CW) is measuredin the direction parallel to support surface 114 (along the Y axis). Thechannel height (CH) is measured in the direction perpendicular tosupport surface 114 (along the Z axis). In some examples, the channelwidth (CW) is constant along the length (the X axis (see, e.g., FIG.2F)) of base 110. In the same or other examples, the channel height (CH)is constant along the length (the X axis) of base 110. In some examples,the channel width (CW) is constant along the channel height (the Z axis)as, for example, shown in FIG. 2A. This type of channel 112 may bereferred to as a straight channel. Alternatively, the channel width (CW)differs along the channel height (the Z axis) as, for example, shown inFIG. 2E. In this example, the channel width (CW) is the greatest atopening 113. This type of channel 112 may be referred to as a taperedchannel and allows for stacking post-forming processing device 100.

Channel 112 is used to accommodate hat portion 191 of pre-curedcomposite stringer 190 when pre-cured composite stringer 190 issupported using post-forming processing device 100. Referring to FIG.2B, hat portion 191 protrudes into channel 112, while flange portions196 rest on support surface 114. It should be noted that the samepost-forming processing device 100 is used for supporting differenttypes of pre-cured composite stringers 190, which may have differentshapes and sizes of hat portions 191. As such, the channel width (CW) islarger than the width of hat portions 191 of pre-cured compositestringers 190 or, more specifically, larger than the width of the widesthat portion 191 among all pre-cured composite stringers 190, processedon post-forming processing device 100. For purposes of this disclosure,the width of hat portion 191 is defined as the largest width, e.g., whenhat portion 191 has a tapered or curved cross-section. Furthermore, thechannel height is larger than the height of hat portion 191 of pre-curedcomposite stringers 190 or, more specifically, larger than the height ofthe tallest hat portion 191 among all pre-cured composite stringers 190,processed on post-forming processing device 100. In general, thecross-sectional profile of channel 112 is sufficient to accommodate anyhat portion 191 of stringer 190, processed using post-forming processingdevice 100.

While FIGS. 2A-2C illustrate a rectangular cross-sectional profile ofchannel 112, any cross-sectional profile capable of accommodating hatportions 191 of pre-cured composite stringers 190 is within the scope ofthe present disclosure, such as tapered profile shown in FIG. 2E,semi-circular profile, and the like. In some examples, thecross-sectional profile of channel 112 corresponds to thecross-sectional profile of hat portions 191, e.g., both are tapered.

Referring to FIG. 2A, support structure 120 at least partially extendswithin channel 112 and along the length of channel 112. In someexamples, support structure 120 is configured to conform to each hatportion 191 and to retain the cross-sectional shape of that hat portion191 when pre-cured composite stringers 190 is supported by and processedusing post-forming processing device 100. It should be noted that thesame support structure 120 is used for different types and profiles ofhat portion 191. Support structure 120 is able to conform to thesedifferent types and profiles while providing sufficient support.

In some examples, support structure 120 is formed from an elasticmaterial, configured to change the shape when conforming to differenttypes of hat portions 191. Some examples of suitable elastic materialsinclude, but are not limited to, latex, silicone (e.g., peroxide orplatinum cured silicon), and other like materials. Some considerationsfor material selection includes weight, clean-ability, solventresistance, stiffness, tear strength, elongation to failure, andhardness.

In some examples, support structure 120 is attached to base 110 at sidewalls of channel 112 as, e.g., is schematically shown in FIG. 1A. Inthese examples, support surface 114 remains exposed and available forinterfacing with flange portions 196 of pre-cured composite stringers190. In other words, support structure 120 does not interfere whenflange portions 196 are positioned on support surface 114, e.g.,compressed between support surface 114 and cover 130. These examples areschematically shown in FIGS. 2A and 2B.

In some examples, support structure 120 comprises a jamming material ora plastically deformable material. For purposes of this disclosure, ajamming material is defined as a material that is able to change itsshape at one condition and to retain its shape at another condition.More specifically, support structure 120 is co-formed or co-shaped withone of pre-cured composite stringers 190 and then retains the shape ofthis stringer while supporting this stringer. For example, the shape ofsupport structure 120 is initially different than that of pre-curedcomposite stringer 190. It should be noted that at this stage pre-curedcomposite stringer 190 is not yet formed. Both support structure 120 anda composite layup are loaded into a forming device, various examples ofwhich are described below, and the shape of support structure 120 isadjusted, while pre-cured composite stringer 190 is being formed. Hence,support structure 120 is co-formed or co-shaped with pre-cured compositestringer 190.

This shape is retained by support structure 120 during various operationof post-forming processing device 100 while supporting this particularstringer. In some examples, the shape is retained while processingmultiple stringers of the same type, e.g., the same cross-sectionalshape of hat portions. When a different type of stringer is to besupported, the shape of support structure 120 is changed, e.g., byco-forming or shaping with that other stringer. These examples areschematically shown in FIGS. 3A and 3B.

Referring to FIG. 3A, in some examples, support structure 120 comprisessupport flanges 124 extending over support surface 114 of base 110 andoutside channel 112. Similar to a portion of support structure 120,extending into channel 112 and supporting hat portions 191 of stringer190, support flanges 124 are specifically shaped to support flangeportions 196 of stringer 190. In some examples, the shape of supportflanges 124 is different from the shape of support surface 114.Therefore, the same post-forming processing device 100 may be used forsupporting stringers with different shapes of flange portions.

In some examples, support structure 120 is removable from base 110. Forexample, support structure 120 is removed from base 110 to change theshape of support structure 120, e.g., when support structure 120 isformed from a jamming material. In some examples, different types ofsupport structure 120 are used with the same base 110.

Cover 130 is configured to attach to base 110, such that thecorresponding one of pre-cured composite stringers 190 is positionedbetween cover 130 and base 110 while supported by post-formingprocessing device 100. More specifically, flange portions 196 ofpre-cured composite stringer 190 are positioned and, in some examples,are compressed between cover 130 and support surface 114 as, forexample, is schematically shown in FIG. 3C. Cover 130 is configured toseal against base 110. Specifically, cover 130 comprises vacuum seal132, which engages seal receiver 115.

In some examples, base 110 comprises pass-through 116, fluidicallycoupled with channel 112 and configured to control pressure insidechannel 112 and under support structure 120. For example, pass-through116 is used to maintain the pressure under support structure 120 to bethe same as in the environment, e.g., when hat portion 191 of pre-curedcomposite stringer 190 is inserted into channel 112 and engages supportstructure 120 or, more specifically, when hat portion 191 pushes supportstructure 120 deeper into channel 112 thereby reducing the volume undersupport structure 120.

In some examples, post-forming processing device 100 further comprisesflexible insert 140 as, e.g., shown in FIG. 2D. Flexible insert 140 ispositioned with channel 112 and under support structure 120 and is usedto provide additional support to hat portion 191. Flexible insert 140allows using support structure 120 that are very flexible and able toconform to a larger variation of hat portion 191 than, for example, whensupport structure 120 is used without flexible insert 140. In someexamples, flexible insert 140 is made from an elastomeric rubber, suchas MOSITES® rubber, latex, or something similar.

Referring to FIG. 2F, in some examples, post-forming processing device100 comprises pass-through bladder seal 180 and dead end bladder seal182. It should be noted that bladder 520, which is further describedbelow with reference to FIGS. 5D-E, is a tube made, e.g., from silicone,VITON®, or other like materials. In some examples, the material ofbladder 520 is reinforced or layered. During processing, bladder 520 isvented to the autoclave atmosphere during cure and vented to the ambientatmosphere during any compaction/vacuum bag. As such, in some examples,one end of bladder 520 comprises a fitting with a vent hole.Pass-through bladder seal 180, shown in FIG. 2F, connects this fittingallowing bladder 520 to vent, when bladder 520 is inside post-formingprocessing device 100. In some examples, post-forming processing device100 comprises pass-through bladder seals on both ends.

Examples of Methods of Fabricating Composite Stringer

FIG. 4 is a process flowchart corresponding to method 400 of fabricatingcomposite stringer 198, see, e.g., FIG. 1B, in accordance with someexamples. Composite stringer 198 should be differentiated from pre-curedcomposite stringer 190, which is an intermediate structure used to formcomposite stringer 198. As such, in some examples, pre-cured compositestringer 190 and composite stringer 198 have the same size and shape.Therefore, FIGS. 1C-1E are representative of both pre-cured compositestringer 190 and composite stringer 198. In some examples, compositestringer 198 comprises a fiber reinforced composite material, which maybe also referred to as a reinforced composite material. This type ofmaterial comprises one or more non-homogeneous polymer-based componentsand one or more non-polymeric based components (e.g., carbon-fibers).Method 400 is described in greater detail below with reference to FIG. 4and FIGS. 5A-H.

Method 400 comprises forming (block 410) pre-cured composite stringer190, e.g., using composite layup 502. This operation is performed usingforming device 510 (shown in FIGS. 5A and 5B), which is different frompost-forming processing device 100, used in later operation (shown inFIGS. 5C-5F). As noted above, post-forming processing device 100increases throughput of forming device 510 since various lateroperations are performed using post-forming processing device 100.

In some examples, composite layup 502 comprises an uncuredpre-impregnated reinforcing tape or fabric, which may be referred to asa prepreg. The tape or fabric comprises fibers, such as graphite fibers,embedded within a matrix material, such as a polymer or, morespecifically, an epoxy or phenolic resin. In some examples, the tape orfabric is unidirectional or woven depending on the design and the degreeof reinforcement desired in the resulting composite stringer 198.

During the forming operation (block 410), composite layup 502 ispositioned on forming device 510 as, e.g., is shown in FIG. 5A. In someexamples, support structure 120 is positioned between composite layup502 and forming device 510, e.g., when support structure 120 isco-formed together with pre-cured composite stringer 190. These examplesare further described below with reference to block 412. Forming device510 comprises forming base 511 with forming cavity 512, which definesthe shape of hat portion 191 of pre-cured composite stringer. Referringto FIG. 5B, forming device 510 also comprises forming die 513, whichpushes a part of composite layup 502 into forming cavity 512 and againstthe walls of forming cavity 512.

Upon completion of this operation, composite layup 502 is formed intopre-cured composite stringer 190. Pre-cured composite stringer 190comprises hat portion 191, which is disposed between forming die 513 andthe walls of forming cavity 512. Pre-cured composite stringer 190 alsocomprises flange portions 196, which extend outside of forming cavity512 and, e.g., conform to forming surface 514 of forming base 511. Insome examples, forming die 513 comprises specially configured bladders,pressing on flange portions 196. These bladders are pressurized andcontact flange portions 196 prior to forming hat portion 191, in someexamples to different pressure level to allow composite layup 502 toslip on forming surface 514 while hat portion 191 is being formed.

In some examples, forming pre-cured composite stringer 190 on formingdevice comprises forming (block 412) support structure 120 ofpost-forming processing device 100. For example, support structure 120comprises a jamming material, various examples and features of which aredescribed above. In some examples, support structure 120 is shaped in aseparate operation from pre-cured composite stringer 190. Alternatively,support structure 120 and pre-cured composite stringer 190 are co-formedor co-shaped in the same overall operation, e.g., the operationrepresented by block 412 is a part of the operation represented by block410, as shown in FIG. 4 . In other words, support structure 120 isplaced into forming device 510 together with composite layup 502. Atthis stage, the shape of support structure 120 is different than theshape of pre-cured composite stringer 190, which will be formed on anddefined by forming device 510. For example, support structure 120 hasbeen previously used for supporting another pre-cured compositestringer, which has a different shape. During concurrent operationsrepresented by block 410 and block 412, pre-cured composite stringer 190is formed while support structure 120 is also co-formed or co-shaped.This support structure forming operation (block 412) may be alsoreferred to as a shape changing operation.

In some examples, method 400 also comprises trimming of pre-curedcomposite stringer 190, e.g., cutting a portion of pre-cured compositestringer 190. For example, an ultrasonic knife is used for cutting.

Method 400 proceeds with transferring (block 420) pre-cured compositestringer 190 from forming device 510 to post-forming processing device100. For instance, the transfer of pre-cured composite stringer 190 fromforming device 510 to post-forming processing device 100 is shown inFIGS. 5B-5C. Various examples of post-forming processing device 100 aredescribed above. In some examples, pre-cured composite stringer 190 istransferred unsupported. Alternatively, pre-cured composite stringer 190is transferred together with support structure 120.

In some examples, the transferring operation comprises controllingpressure inside channel 112 of base 110. For example, inserting hatportion 191 of pre-cured composite stringer 190 into channel 112 maycause displacing of air from channel 112, e.g., through pass-through116.

In some examples, the transferring operation comprises stretching (block422) support structure 120 of post-forming processing device 100. Inthese examples, support structure 120 is formed from an elastic materialthat conforms to the shape of hat portion 191 of pre-cured compositestringer 190 as hat portion is inserted into channel 112. Morespecifically, the elastic material is configured to change the shapewhen conforming to each of hat portions 191. As noted above, in someexamples, hat portions 191 have different cross-sectional shapes. Thisstretching feature as, e.g., is shown in FIGS. 2A-2B, of supportstructure 120 allows supporting pre-cured composite stringers 190 withdifferent sizes of hat portions 191.

In some examples, the transferring operation comprises adjusting (block424) the shape of post-forming processing device 100. FIGS. 6A and 6Billustrate base 110 of post-forming processing device 100, which has apivot point, defined by first axis 601. Other components of post-formingprocessing device 100, such as support structure 120, are not shown forsimplicity. The pivot point allows base 110 to have an in-plane bendingand accommodate both straight pre-cured composite stringers (in theconfiguration shown in FIG. 6A) and pre-cured composite stringers withan in-plane bend (in the configurations shown in FIG. 6B). While onlyone pivot point is shown in FIGS. 6A and 6B, one having ordinary skillin the art would understand that any number of pivot points may bepresent. Furthermore, in some examples, post-forming processing device100 has an out-of-plane bending functionality. It should be noted thatsome degrees of bending, especially localized bending, of pre-curedcomposite stringers can be accommodated by the side of channel 112within base 110, without bending base 110.

In some examples, method 400 comprises inspecting (block 430) pre-curedcomposite stringer 190. The inspection is performed while pre-curedcomposite stringer 190 is positioned on post-forming processing device100. For example, the inspection involves checking the surface ofpre-cured composite stringer 190 for wrinkles, bubbles, foreign objectdebris (FOD), loose fibers, wrinkles, and shape. It should be noted thatthe inspection operation is performed away from forming device 510 andcuring device 540, thereby allowing other pre-cured composite stringersto be processes on these devices and increasing the overall processthroughput.

Method 400 comprises installing (block 440) bladder 520 on pre-curedcomposite stringer 190 as, e.g., schematically shown in FIG. 5D. Bladder520 is installed while pre-cured composite stringer 190 is positioned onpost-forming processing device 100. In some example, bladder 520 iswrapped into a bladder warp, which is later cured into the skin of thestringer when bladder 520 is removed. Bladder 520 is used during curingoperation to provide support inside of pre-cured composite stringer 190.In some examples, bladder 520 is a solid object composed of silicone,urethane, or similar materials, including any combination thereof. Insome examples, bladder 520 is shaped to substantially correspond withpre-cured composite stringer 190.

Method 400 comprises installing (block 450) noodle 530 at an interfacebetween bladder 520 and pre-cured composite stringer 190 and within theplane of support surface 114 of base 110 as, e.g., schematically shownin FIG. 5E. This installing operation is performed while pre-curedcomposite stringer 190 is positioned on post-forming processing device100. Noodle 530 is also referred to as a radius filler.

In some examples, method 400 comprises compacting (block 460) pre-curedcomposite stringer 190, while pre-cured composite stringer 190 ispositioned on post-forming processing device 100. For example, thecompacting operation involves sealing cover 130 of post-formingprocessing device 100 against base 110 of post-forming processing device100 as, for example, is schematically shown in FIG. 5F. In someexamples, the compacting operation further comprises contacting at leastflange portions 196 of pre-cured composite stringer 190 with cover 130of post-forming processing device 100.

In some examples, method 400 comprises staging and transportingpre-cured composite stringer 190. These operations are performed whilepre-cured composite stringer 190 is positioned on post-formingprocessing device 100. Furthermore, post-forming processing device 100is used for storing pre-cured composite stringer 190, while providingsupport to pre-cured composite stringer 190.

Method 400 proceeds with transferring (block 490) pre-cured compositestringer 190 from post-forming processing device 100 to curing device540. For instance, the transfer of pre-cured composite stringer 190 frompost-forming processing device 100 to curing device 540 is shown in FIG.5F-5H. In some examples, pre-cured composite stringer 190 is transferredtogether with bladder 520 and/or noodle 530, which are installed ontopre-cured composite stringer 190 while pre-cured composite stringer 190was positioned on post-forming processing device 100.

Method 400 comprises curing (block 492) pre-cured composite stringer 190on curing device 540, thereby forming composite stringer 198 as, forexample, is schematically shown in FIGS. 5H and 5I. For example,pre-cured composite stringer 190, shown in FIG. 5H, is subjected to heatand pressure to cross-link the resin within pre-cured composite stringer190. Unlike pre-cured composite stringer 190, composite stringer 198,shown in FIG. 5I, does not require the level of support needed forpre-cured composite stringer 190. As such, post-forming processingdevice 100 is not used for composite stringer 198.

In some examples, various operations of method 400 are repeated(decision block 494) with additional pre-cured composite stringer 199,e.g., one example of which is shown in FIG. 1E. Specifically, additionalpre-cured composite stringer 199 has a different design than pre-curedcomposite stringer 190, previously processed using the same post-formingprocessing device 100. Various different designs for pre-cured compositestringers are shown in FIGS. 1C-1E. Other example designs for thepre-cure composite stringer are possible as well.

Specifically, method 400 comprises forming 410 an additional pre-curedcomposite stringer 199 on an additional forming device. Unlikepost-forming processing device 100, which can be universally used acrossa variety of different designs of pre-cured composite stringers, formingdevices are dedicated tools. In some examples, support structure 120 isreformed or reshaped during this operation of forming additionalpre-cured composite stringer 199. More specifically, support structure120 has a different shape when supporting additional pre-cured compositestringer 199 than when supporting pre-cured composite stringer 190.

Method 400 proceeds with transferring (block 420) this additionalpre-cured composite stringer 199 from the forming device to post-formingprocessing device 100. As noted above, additional pre-cured compositestringer 199 has a different design and, more specifically, a differentcross-sectional profile than pre-cured composite stringer 190.

In some examples, method 400 continues with installing an additionalbladder on additional pre-cured composite stringer 199, while additionalpre-cured composite stringer 199 is positioned on post-formingprocessing device 100. Furthermore, a noodle is installed on additionalpre-cured composite stringer 199, while additional pre-cured compositestringer 199 is positioned on post-forming processing device 100.However, these operations are optional.

Method 400 proceeds with transferring additional pre-cured compositestringer 199 together with additional bladder and additional noodle frompost-forming processing device 100 to an additional curing device andcuring pre-cured composite stringer 190 using additional curing device,thereby forming an additional composite stringer.

FIG. 7 is a process flowchart of method 700 of supporting pre-curedcomposite stringer 190 using post-forming processing device 100, inaccordance with some examples of the present disclosure. Method 700comprises transferring (block 720) pre-cured composite stringer 190 topost-forming processing device 100 as, for example, is schematicallyshown in FIG. 5C. Various examples of pre-cured composite stringer 190are described above. For example, pre-cured composite stringer 190comprises comprising hat portion 191, which is supported upon thetransfer of pre-cured composite stringer 190 to post-forming processingdevice 100. Post-forming processing device 100 comprises base 110,comprising channel 112. Post-forming processing device 100 alsocomprises support structure 120, at least partially extending withinchannel 112 and along the length of channel 112.

When pre-cured composite stringer 190 is transferred to post-formingprocessing device 100, support structure 120 conforming to hat portion191 of pre-cured composite stringer 190, as for, example, isschematically shown in FIG. 5C. More specifically, support structure 120retains the cross-sectional shape of hat portion 191 of pre-curedcomposite stringer 190 while pre-cured composite stringer 190 ispositioned in post-forming processing device 100. In some examples,support structure 120 is formed from a flexible material, providing thisconformal supports. In other examples, support structure 120 is madefrom a jamming material that is reshaped together with each newpre-cured composite stringer.

In some examples, the transferring operation (block 720) comprisesstretching (block 722) support structure 120 of post-forming processingdevice 100 as, for example, is schematically shown in FIGS. 2A-2B. Inthese examples, support structure 120 is formed from an elastic materialthat conforms to the shape of hat portion 191 of pre-cured compositestringer 190 as hat portion is inserted into channel 112. Thisstretching feature of support structure 120 allows supporting pre-curedcomposite stringers 190 with different sizes of hat portions 191.

In some examples, the transferring operation (block 720) comprisesadjusting (block 724) the shape of post-forming processing device 100.FIGS. 6A and 6B illustrate base 110 of post-forming processing device100, which has a pivot point, defined by first axis 601. Othercomponents of post-forming processing device 100, such as supportstructure 120, are not shown for simplicity. The pivot point allows base110 to have an in-plane bending and accommodate both straight pre-curedcomposite stringers (in the configuration shown in FIG. 6A) andpre-cured composite stringers with an in-plane bend (in theconfigurations shown in FIG. 6B). While only one pivot point is shown inFIGS. 6A and 6B, one having ordinary skill in the art would understandthat any number of pivot points may be present. Furthermore, in someexamples, post-forming processing device 100 has an out-of-plane bendingfunctionality. It should be noted that some degrees of bending,especially localized bending, of pre-cured composite stringers can beaccommodated by the side of channel 112 within base 110, without bendingbase 110.

In some examples, the transferring operation (block 720) comprisespositioning (block 726) cover 130 of post-forming processing device 100against base 110 of post-forming processing device 100 as, for example,is schematically shown in FIG. 5F. In some examples, cover 130 is sealedagainst base 110. Furthermore, in some examples, this cover positioningoperation (block 726) compacts at least flange portions 196 of pre-curedcomposite stringer 190.

In some examples, the transferring operation (block 720) comprisescontrolling (block 728) pressure inside channel 112 of base 110. Forexample, inserting hat portion 191 of pre-cured composite stringer 190into channel 112 may cause displacing of air from channel 112, e.g.,through pass-through 116.

In some examples, method 700 comprises storing (block 730) pre-curedcomposite stringer 190. More specifically, pre-cured composite stringer190 is stored in post-forming processing device 100 prior to removing(block 740) pre-cured composite stringer 190 from post-formingprocessing device 100.

Method 700 proceeds with removing (block 740) pre-cured compositestringer 190 from post-forming processing device 100. For example,pre-cured composite stringer 190 is transferred to curing device 540 as,for example, is schematically shown in FIG. 5H. Alternatively, pre-curedcomposite stringer 190 is transferred to other equipment, e.g., forinspection.

Method 700 proceeds or, more specifically repeats, (decision block 794)with transferring (block 720) additional pre-cured composite stringer199 to post-forming processing device 100 as, for example, isschematically shown in FIG. 5J. Additional pre-cured composite stringer199 comprising additional hat portion 193, such that cross-sectionalshape of additional hat portion 193 of additional pre-cured compositestringer 199, different from the cross-sectional shape of hat portion191 of pre-cured composite stringer 190, shown in FIG. 5C. However,despite this difference in the cross-sectional shapes, support structure120 of post-forming processing device 100 conforms to additional hatportion 193 of additional pre-cured composite stringer 199. Furthermore,support structure 120 retains the cross-sectional shape of additionalhat portion 193 of additional pre-cured composite stringer 199.

Aircraft Examples

In some examples, methods and systems described above are used onaircraft and, more generally, by the aerospace industry. Specifically,these methods and systems can be used during fabrication of aircraft aswell as during aircraft service and maintenance.

Accordingly, the apparatus and methods described above are applicablefor aircraft manufacturing and service method 900 as shown in FIG. 8 andfor aircraft 902 as shown in FIG. 9 . During pre-production, method 900includes specification and design 904 of aircraft 902 and materialprocurement 906. During production, component and subassemblymanufacturing 908 and system integration 910 of aircraft 902 takesplace. Thereafter, aircraft 902 goes through certification and delivery912 in order to be placed in service 914. While in service by acustomer, aircraft 902 is scheduled for routine maintenance and service916, which also includes modification, reconfiguration, refurbishment,and so on.

In some examples, each of the processes of method 900 is performed orcarried out by a system integrator, a third party, and/or an operator,e.g., a customer. For the purposes of this description, a systemintegrator includes without limitation any number of aircraftmanufacturers and major-system subcontractors; a third party includeswithout limitation any number of venders, subcontractors, and suppliers;and an operator can be an airline, leasing company, military entity,service organization, and so on.

As shown in FIG. 9 , aircraft 902 produced by method 900 includesairframe 918 with plurality of systems 920, and interior 922. Examplesof systems 920 include one or more of propulsion system 924, electricalsystem 926, hydraulic system 928, and environmental system 930. Anynumber of other systems can be included. Although an aerospace exampleis shown, the principles of the examples described herein is applied toother industries, such as the automotive industry.

Apparatus and methods presented herein can be employed during any one ormore of the stages of method 900. For example, components orsubassemblies corresponding to manufacturing 908 are fabricated ormanufactured in a manner similar to components or subassemblies producedwhile aircraft 902 is in service. Also, one or more apparatus examples,method examples, or a combination thereof is utilized duringmanufacturing 908 and system integration 910, for example, bysubstantially expediting assembly of or reducing the cost of an aircraft902. Similarly, one or more of apparatus examples, method examples, or acombination thereof is utilized while aircraft 902 is in service, forexample and without limitation, to maintenance and service 916.

Further Examples

Further, description includes examples according to following clauses:

Clause 1. A post-forming processing device for supporting pre-curedcomposite stringers, comprising hat portions, having cross-sections,different among the pre-cured composite stringers, the post-formingprocessing device comprising:

-   -   a base, comprising a channel, having a channel width and a        channel height, wherein:        -   the channel width is larger than a width of the hat portions            of the pre-cured composite stringers, and        -   the channel height is larger than heights of the hat            portions of the pre-cured composite stringers;    -   a support structure, at least partially extending within the        channel and along a length of the channel and configured to        conform to each of the hat portions and to retain a        cross-sectional shape of each of the hat portions when a        corresponding one of the pre-cured composite stringers is        supported by the post-forming processing device; and    -   a cover, configured to attach to the base, such that the        corresponding one of the pre-cured composite stringers is        positioned between the cover and the base while supported by the        post-forming processing device.

Clause 2. The post-forming processing device of clause 1, wherein thesupport structure is formed from an elastic material configured tochange shape when conforming to each of the hat portions.

Clause 3. The post-forming processing device of clause 2, wherein thesupport structure is attached to the base at side walls of the channel.

Clause 4. The post-forming processing device of any one of clauses 1-3,wherein the support structure comprises a jamming material or aplastically deformable material.

Clause 5. The post-forming processing device of clause 4, wherein thesupport structure is co-formed with the corresponding one of thepre-cured composite stringers.

Clause 6. The post-forming processing device of clause 4, wherein thesupport structure comprises support flanges extending over a supportsurface of the base and outside the channel.

Clause 7. The post-forming processing device of clause 4, wherein thesupport structure is removable from the base.

Clause 8. The post-forming processing device of any one of clause 1-7,wherein the base comprising a pass-through, fluidically coupled with thechannel and configured to control pressure inside the channel.

Clause 9. The post-forming processing device of any one of clauses 1-8,further comprising a flexible insert, positioned with the channel andunder the support structure.

Clause 10. The post-forming processing device of any one of clause 1-10,wherein the cover is configured to seal against the base.

Clause 11. A method of fabricating a composite stringer, the methodcomprising:

-   -   forming a pre-cured composite stringer on a forming device, the        pre-cured composite stringer comprising a hat portion;    -   transferring the pre-cured composite stringer from the forming        device to a post-forming processing device, comprising:        -   a base, comprising a channel, and        -   a support structure, at least partially extending within the            channel and along a length of the channel and conforming to            the hat portion and retaining a cross-sectional shape of the            hat portion; and    -   installing a bladder on the pre-cured composite stringer, while        the pre-cured composite stringer is positioned on the        post-forming processing device;    -   installing a noodle at an interface between the bladder and the        pre-cured composite stringer and within a plane of a support        surface of the base, while the pre-cured composite stringer is        positioned on the post-forming processing device;    -   transferring the pre-cured composite stringer together with the        bladder and the noodle from the post-forming processing device        to a curing device; and    -   curing the pre-cured composite stringer on the curing device,        thereby forming the composite stringer.

Clause 12. The method of clause 11, further comprising inspecting thepre-cured composite stringer, while the pre-cured composite stringer ispositioned on the post-forming processing device.

Clause 13. The method of any one of clauses 11-12, further comprisingcompacting the pre-cured composite stringer, while the pre-curedcomposite stringer is positioned on the post-forming processing device.

Clause 14. The method of clause 13, wherein compacting the pre-curedcomposite stringer comprises sealing a cover of the post-formingprocessing device against the base of the post-forming processingdevice.

Clause 15. The method of clause 14, wherein compacting the pre-curedcomposite stringer further comprises contacting at least flange portionsof the pre-cured composite stringer with the cover of the post-formingprocessing device.

Clause 16. The method of any one of any one of clauses 11-15, whereinforming the pre-cured composite stringer on the forming device comprisesforming the support structure of the post-forming processing device.

Clause 17. The method of any one of clauses 11-16, wherein transferringthe pre-cured composite stringer from the forming device to thepost-forming processing device comprises controlling pressure inside thechannel of the base.

Clause 18. The method of any one of clause 11-17, wherein transferringthe pre-cured composite stringer from the forming device to thepost-forming processing device comprises stretching the supportstructure of the post-forming processing device.

Clause 19. The method of any one of clauses 11-18, further comprising:

-   -   forming an additional pre-cured composite stringer on an        additional forming device;    -   transferring the additional pre-cured composite stringer from        the forming device to the post-forming processing device,        wherein the additional pre-cured composite stringer has a        different cross-sectional profile from the pre-cured composite        stringer;    -   installing an additional bladder on the additional pre-cured        composite stringer, while the additional pre-cured composite        stringer is positioned on the post-forming processing device;    -   installing an additional noodle on the additional pre-cured        composite stringer, while the additional pre-cured composite        stringer is positioned on the post-forming processing device;    -   transferring the additional pre-cured composite stringer        together with the additional bladder and the additional noodle        from the post-forming processing device to an additional curing        device; and    -   curing the pre-cured composite stringer using the additional        curing device, thereby forming an additional composite stringer.

Clause 20. The method of clause 19, wherein the support structure has adifferent shape when supporting the additional pre-cured compositestringer than when supporting the pre-cured composite stringer.

Clause 21. A method comprising:

-   -   transferring a pre-cured composite stringer, comprising a hat        portion, to a post-forming processing device, comprising:        -   a base, comprising a channel, and        -   a support structure, at least partially extending within the            channel and along a length of the channel and conforming to            the hat portion of the pre-cured composite stringer and            retaining a cross-sectional shape of the hat portion of the            pre-cured composite stringer; and    -   removing the pre-cured composite stringer from the post-forming        processing device;        and    -   transferring an additional pre-cured composite stringer,        comprising an additional hat portion, to the post-forming        processing device, wherein the support structure of the        post-forming processing device conforms to the additional hat        portion of the additional pre-cured composite stringer and        retains a cross-sectional shape of the additional hat portion of        the additional pre-cured composite stringer, different from the        cross-sectional shape of the hat portion of the pre-cured        composite stringer.

Clause 22. The method of clause 21, wherein transferring the pre-curedcomposite stringer comprises positioning a cover of the post-formingprocessing device against the base of the post-forming processingdevice.

Clause 23. The method of any one of clauses 21-22, wherein transferringthe pre-cured composite stringer to the post-forming processing devicecomprises controlling pressure inside the channel of the base.

Clause 24. The method of any one of clause 21-23, wherein transferringthe pre-cured composite stringer to the post-forming processing devicecomprises stretching the support structure of the post-formingprocessing device.

Clause 25. The method of any one of clauses 21-24, wherein thepost-forming processing device is used for storing the pre-curedcomposite stringer prior to removing the pre-cured composite stringerfrom the post-forming processing device.

CONCLUSION

Although the foregoing concepts have been described in some detail forpurposes of clarity of understanding, it will be apparent that certainchanges and modifications may be practiced within the scope of theappended claims. It should be noted that there are many alternative waysof implementing the processes, systems, and apparatus. Accordingly, thepresent examples are to be considered as illustrative and notrestrictive.

What is claimed is:
 1. A method of fabricating a plurality of compositestringers, the method comprising: forming a plurality of pre-curedcomposite stringers on a forming device, the pre-cured compositestringers comprising different hat portions having differentcross-section shapes; and transferring each of the pre-cured compositestringers from the forming device to a post-forming processing device,comprising: a base, comprising a channel, and a support structure, atleast partially extending within the channel and along a length of thechannel and conforming to each hat portion and being reshaped for eachdifferent cross-section shape of each hat portion.
 2. The method ofclaim 1, further comprising inspecting each pre-cured compositestringer, while each pre-cured composite stringer is positioned on thepost-forming processing device.
 3. The method of claim 1, furthercomprising compacting each pre-cured composite stringer, while eachpre-cured composite stringer is positioned on the post-formingprocessing device.
 4. The method of claim 3, wherein compacting eachpre-cured composite stringer comprises sealing a cover of thepost-forming processing device against the base of the post-formingprocessing device.
 5. The method of claim 4, wherein compacting eachpre-cured composite stringer further comprises contacting at leastflange portions of the pre-cured composite stringer with the cover ofthe post-forming processing device.
 6. The method of claim 1, whereinforming each pre-cured composite stringer on the forming devicecomprises forming the support structure of the post-forming processingdevice.
 7. The method of claim 1, wherein transferring each pre-curedcomposite stringer from the forming device to the post-formingprocessing device comprises controlling pressure inside the channel ofthe base.
 8. The method of claim 1, wherein transferring each pre-curedcomposite stringer from the forming device to the post-formingprocessing device comprises stretching the support structure of thepost-forming processing device.
 9. The method of claim 1, furthercomprising: installing a bladder on a first one of the pre-curedcomposite stringers, while the first pre-cured composite stringer ispositioned on the post-forming processing device; and installing anoodle at an interface between the bladder and the first pre-curedcomposite stringer and within a plane of a support surface of the base,while the first pre-cured composite stringer is positioned on thepost-forming processing device.
 10. The method of claim 9, furthercomprising: transferring the first pre-cured composite stringer togetherwith the bladder and the noodle from the post-forming processing deviceto a curing device; and curing the first pre-cured composite stringer onthe curing device, thereby forming a first composite stringer.
 11. Themethod of claim 1, wherein the support structure is formed from anelastic material configured to change shape to conform to at least aside portion and a base portion of each of the hat portions' differentcross-section shape when conforming to each of the hat portions.
 12. Themethod of claim 1, wherein the support structure is attached to the baseat side walls of the channel.
 13. The method of claim 1, wherein thesupport structure comprises a jamming material or a plasticallydeformable material.
 14. The method of claim 1, wherein the supportstructure is co-formed with each corresponding one of the pre-curedcomposite stringers.
 15. The method of claim 1, wherein the supportstructure is configured to conform to at least a side portion and abottom portion of each of the hat portions when a corresponding one ofthe pre-cured composite stringers is supported by the post-formingprocessing device.
 16. A method of fabricating a plurality of compositestringers, the method comprising: transferring a first pre-curedcomposite stringer, comprising a first hat portion having a firstcross-section shape to a post-forming processing device, comprising: abase, comprising a channel, and a support structure, at least partiallyextending within the channel and along a length of the channel andconforming to the first hat portion of the first pre-cured compositestringer and being reshaped to the first cross-section shape of thefirst hat portion of the first pre-cured composite stringer; andremoving the first pre-cured composite stringer from the post-formingprocessing device; and transferring a second pre-cured compositestringer, comprising a second hat portion having a second cross-sectionshape, which differs from the first cross-section shape, to thepost-forming processing device, wherein: the support structure of thepost-forming processing device conforms to the second hat portion of thesecond pre-cured composite stringer and is reshaped to the secondcross-section shape of the second hat portion of the second pre-curedcomposite stringer.
 17. The method of claim 16, wherein transferring thefirst pre-cured composite stringer comprises positioning a cover of thepost-forming processing device against the base of the post-formingprocessing device.
 18. The method of claim 16, wherein transferring thefirst pre-cured composite stringer to the post-forming processing devicecomprises controlling pressure inside the channel of the base.
 19. Themethod of claim 16, wherein transferring the first pre-cured compositestringer to the post-forming processing device comprises stretching thesupport structure of the post-forming processing device.
 20. The methodof claim 16, wherein the post-forming processing device is used forstoring the first pre-cured composite stringer prior to removing thefirst pre-cured composite stringer from the post-forming processingdevice.